Results 11 to 20 of about 148,925 (251)

On reachability of nominal aircraft flight dynamics by data-based control reconfiguration in case of actuator failures [PDF]

open access: yesE3S Web of Conferences, 2023
The paper proposes the data-based method for reaching and maintaining the nominal aircraft flight dynamics in in case of actuator failures. The method is based on aircraft control reconfiguration and uses input and output data of flight control system ...
Lapin Alexey   +2 more
doaj   +1 more source

A Coordination Optimization Method for Load Shedding Considering Distribution Network Reconfiguration

open access: yesEnergies, 2022
Load shedding control is an emergency control measure to maintain the frequency stability of the power system. Most of the existing load shedding methods use the extensive form of directly cutting off the outlet of the substation, featuring low control ...
Kai Wang, Lixia Kang, Songhao Yang
doaj   +1 more source

Shipboard Power Management for Failure Mode Using the Hybrid MPC Approach

open access: yesEnergies, 2021
Shipboard integrated power systems, the key technology of ship electrification, call for effective failure mode power management control strategy to achieve the safe and reliable operation in dynamic reconfiguration.
Xiuyan Peng   +3 more
doaj   +1 more source

Continuous Coverage Control of UAVs Based on Cluster Reconfiguration in the Context of Counterattack

open access: yesIEEE Access, 2023
UAV clusters are the main application form of multi-intelligence for the intelligent era. Especially in the context of strikes, UAV clusters become an efficient weapon resource on the battlefield by their flexible mobility, no casualties, and low cost ...
Xinglong Gu   +3 more
doaj   +1 more source

Ship Integrated Power System reconfiguration research under partial observation

open access: yesEnergy Reports, 2022
Shipboard Integrated Power System (IPS) has been considered as the trending technology for future Ships. To ensure the safe and stable operation not only in normal mode, but also when unknown faults occur or other emergency situation, this paper proposes
Zhengzhuo Liang   +4 more
doaj   +1 more source

Hybrid Adaptive Control for Tiltrotor Aircraft Flight Control Law Reconfiguration

open access: yesAerospace, 2023
Tiltrotor aircrafts have both fixed-wing control surfaces and helicopter rotors for attitude control. The redundancy of control surfaces provides the possibility for the control system to reconfigure the control law when actuator faults occur during ...
Jiayu Wen   +4 more
doaj   +1 more source

RECONFIGURATION OF THE AIRCRAFT INTEGRATED CONTROL SYSTEM REGARDING CONTROL CONSTRAINTS UNDER ACTUATOR FAILURES

open access: yesНаучный вестник МГТУ ГА, 2018
The aircraft integrated control system reconfiguration laws under failures of actuators, calculated disregarding physical constraints on control surfaces saturation, can lead to a complete loss of aircraft controllability and stability. Despite the large
A. M. Kulchak   +2 more
doaj   +1 more source

Satellite Cluster Formation Reconfiguration Based on the Bifurcating Potential Field

open access: yesAerospace, 2022
The satellite cluster formation reconfiguration has received considerable attention in recent years. However, the traditional centralized control methods are challenging to apply to satellite clusters because of the enormous fuel consumption, and few ...
Wanying Gao, Kehang Li, Chunling Wei
doaj   +1 more source

Assessment of a Universal Reconfiguration-less Control Approach in Open-Phase Fault Operation for Multiphase Drives [PDF]

open access: yes, 2019
Multiphase drives have been important in particular industry applications where reliability is a desired goal. The main reason for this is their inherent fault tolerance. Di erent nonlinear controllers that do not include modulation stages, like direct
Barrero, Federico   +4 more
core   +2 more sources

Integrated reconfigurable control and guidance based on evaluation of degraded performance [PDF]

open access: yes, 2016
The present paper is focused on analysing an integrated reconfigurable control and guidance approach for recovering a small fixed-wing UAV from different actuator faults, which cover locked in place (stuck) and loss of effectiveness. The model of the UAV
Casaban-Lillo, Conekt   +3 more
core   +1 more source

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